EP3258080A1 - Compresseur de suralimentation - Google Patents

Compresseur de suralimentation Download PDF

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Publication number
EP3258080A1
EP3258080A1 EP15881914.4A EP15881914A EP3258080A1 EP 3258080 A1 EP3258080 A1 EP 3258080A1 EP 15881914 A EP15881914 A EP 15881914A EP 3258080 A1 EP3258080 A1 EP 3258080A1
Authority
EP
European Patent Office
Prior art keywords
component
diffuser
bearing housing
outer peripheral
inner peripheral
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP15881914.4A
Other languages
German (de)
English (en)
Other versions
EP3258080A4 (fr
EP3258080B1 (fr
Inventor
Takashi NAMBU
Hiroshi Suzuki
Takashi Shiraishi
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Heavy Industries Engine and Turbocharger Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Publication of EP3258080A1 publication Critical patent/EP3258080A1/fr
Publication of EP3258080A4 publication Critical patent/EP3258080A4/fr
Application granted granted Critical
Publication of EP3258080B1 publication Critical patent/EP3258080B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C17/00—Sliding-contact bearings for exclusively rotary movement
    • F16C17/04—Sliding-contact bearings for exclusively rotary movement for axial load only
    • F16C17/045—Sliding-contact bearings for exclusively rotary movement for axial load only with grooves in the bearing surface to generate hydrodynamic pressure, e.g. spiral groove thrust bearings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B39/00—Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C35/00—Rigid support of bearing units; Housings, e.g. caps, covers
    • F16C35/02—Rigid support of bearing units; Housings, e.g. caps, covers in the case of sliding-contact bearings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16J—PISTONS; CYLINDERS; SEALINGS
    • F16J15/00—Sealings
    • F16J15/16—Sealings between relatively-moving surfaces
    • F16J15/34—Sealings between relatively-moving surfaces with slip-ring pressed against a more or less radial face on one member
    • F16J15/3436—Pressing means
    • F16J15/3452—Pressing means the pressing force resulting from the action of a spring
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/40—Application in turbochargers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/50—Bearings
    • F05D2240/52—Axial thrust bearings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C17/00—Sliding-contact bearings for exclusively rotary movement
    • F16C17/04—Sliding-contact bearings for exclusively rotary movement for axial load only
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2360/00—Engines or pumps
    • F16C2360/23—Gas turbine engines
    • F16C2360/24—Turbochargers

Definitions

  • This disclosure relates to a turbocharger.
  • the turbocharger includes a rotation shaft and a compressor impeller provided on the rotation shaft on one end side thereof.
  • the intake air is compressed by the compressor impeller provided on the rotation shaft on one end side thereof.
  • the intake air compressed by the compressor impeller flows through a diffuser flow path defined between a compressor housing and a bearing housing, thereby being introduced to a scroll flow path formed in the outer peripheral portion of the compressor housing.
  • the radially outer portion of the compressor impeller is formed to have a size substantially same or larger than that of the radially inner portion of the bearing housing, and a large gap does not exist between the outer peripheral edge of the compressor impeller and the inner peripheral wall surface of the bearing housing.
  • FIG. 1 and the like of Patent Document 1 a technology of preventing the compression efficiency of a turbo compressor from decreasing as follows is disclosed. Specifically, in a turbocharger (turbo compressor 3) in which a seal plate (denoted by 11) is fixed to a bearing housing (bearing housing 7) by a fastening screw (denoted by 21) in a diffuser flow path (diffuser D), an opening end portion of a counterbore (denoted by 20) configured to support the fastening screw is occluded.
  • the turbo compressor of Patent Document 1 has a basic structure different from that of the turbocharger according to one embodiment of this invention described later in that the seal plate is fixed to the end portion of the bearing housing by the fastening screw in the turbo compressor of Patent Document 1.
  • FIG. 2 and the like of Patent Document 2 a technology of preventing the compression efficiency of a compressor impeller from decreasing as follows is disclosed.
  • a turbocharger turbocharger
  • a seal plate denoted by 20
  • a bearing housing denoted by 3
  • a bolt denoted by 21
  • an annular component denoted by 31
  • a diffuser portion denoted by 27
  • the turbocharger of Patent Document 2 has a basic structure different from that of the turbocharger according to one embodiment of this invention described later in that the seal plate is fixed to the end portion of the bearing housing by the bolt in the turbocharger of Patent Document 2.
  • this invention is provided on the basis of the situation of the related-art the technology as above and has an object to provide a turbocharger capable of enhancing the compression efficiency by filling a gap formed between an outer peripheral edge of a compressor impeller and an inner peripheral wall surface of a bearing housing through a simple structure.
  • the diffuser component can be fixed in the bearing housing through a simple structure in which the outer peripheral surface of the diffuser component and the inner peripheral wall surface of the bearing housing are simply threadedly engaged with each other.
  • the turbocharger capable of enhancing the compression efficiency by filling the gap formed between the outer peripheral edge of the compressor impeller and the inner peripheral wall surface of the bearing housing through a simple structure can be provided.
  • the bearing housing and the components accommodated in the bearing housing can be used in common for the turbocharger of the related-art.
  • expressions describing shapes such as a quadrangle and a cylinder not only describe shapes such as a quadrangle and a cylinder in geometrically precise terms, but also describe shapes including recessed portions, projecting portions, chamfered portions, and the like within the range in which the same effect is achieved.
  • FIG. 1 is a sectional side view illustrating the cross section of a turbocharger according to one embodiment of this invention taken along the axial direction of a rotation shaft of the turbocharger.
  • the turbocharger according to one embodiment of this invention is not particularly limited, but is, for example, a turbocharger mounted on an engine for an automobile.
  • a turbocharger 100 of this embodiment includes three housings, that is, a turbine housing 102 configured to accommodate a turbine impeller 103 provided on a rotation shaft 2 on one end side thereof, a compressor housing 104 configured to accommodate a compressor impeller 105 provided on the rotation shaft 2 on the other end side thereof, and a bearing housing 106 configured to accommodate a radial bearing 110 configured to support the rotation shaft 2 in a rotatable manner and a thrust plate 4 configured to support the thrust force (axial force) of the rotation shaft 2.
  • a spiral-shaped turbine scroll flow path 113 is formed at an outer peripheral portion of the turbine housing 102.
  • the turbine impeller 103 is placed at a central part of the turbine scroll flow path 113.
  • the turbine impeller 103 includes a turbine hub 103A having a truncated conical shape formed by cutting off a top portion of a cone along a plane parallel to the base thereof, and a plurality of turbine blades 103B provided to radially protrude from the peripheral surface of the turbine hub 103A.
  • the turbine hub 103A of the turbine impeller 103 is bonded to one end portion of the rotation shaft 2 by welding, for example.
  • Exhaust gas flowing through the turbine scroll flow path 113 and acting on the turbine impeller 103 is discharged to the outside of the turbine housing 102 from an exhaust gas discharging flow path 111 extending along the axial direction of the rotation shaft 2.
  • a spiral-shaped compressor scroll flow path 117 is formed at an outer peripheral portion of the compressor housing 104.
  • the compressor impeller 105 is placed at a central part of the compressor scroll flow path 117.
  • the compressor impeller 105 includes a compressor hub 105A having a truncated conical shape formed by cutting off a top portion of a cone along a plane parallel to the base thereof, and a plurality of compressor blades 105B provided to radially protrude from the peripheral surface of the compressor hub 105A.
  • An insertion hole (not shown) to which the other end side of the rotation shaft 2 is inserted is formed at a central part of the compressor hub 105A of the compressor impeller 105.
  • the compressor impeller 105 is fixed to the other end portion of the rotation shaft 2 by inserting one end side of the rotation shaft 2 into the insertion hole and fastening a nut 116 from the tip of the compressor hub 105A.
  • Intake air flowing through an intake air introducing flow path 115 extending along the axial direction of the rotation shaft 2 and compressed by the compressor impeller 105 is introduced to the compressor scroll flow path 117 via a diffuser flow path 112 extending along the direction orthogonal to the axis of the rotation shaft 2, and is supplied to an engine (not shown).
  • the bearing housing 106 is placed between the turbine housing 102 and the compressor housing 104.
  • the bearing housing 106 is connected, at an end portion on one side thereof, to the compressor housing 104, and connected, at an end portion on the other side thereof, to the turbine housing 102.
  • the diffuser flow path 112 described above is defined between the bearing housing 106 and the compressor housing 104.
  • a protruding wall portion 106A protruding from an inner peripheral wall surface 106a of the bearing housing 106 is formed in the bearing housing 106.
  • a lubricant oil introducing path 118 configured to introduce lubricant oil to be supplied to the radial bearing 110 and the thrust plate 4 described above is formed in the protruding wall portion 106A.
  • the lubricant oil introduced into the bearing housing 106 from the lubricant oil introducing path 118 lubricates the radial bearing 110 and the thrust plate 4 and is discharged to the outside of the bearing housing 106 from a lubricant oil outlet 119 formed in a lower part of the bearing housing 106.
  • FIG. 2A , FIG. 3A , FIG. 4A , FIG. 5A , FIG. 6A , FIG. 7A , FIG. 8A , and FIG. 9A each are a sectional view of the main part of a turbocharger according to one embodiment of this invention.
  • FIG. 2B , FIG. 3B , FIG. 4B , FIG. 5B , FIG. 6B , FIG. 7B , FIG. 8B , and FIG. 9B each are a view illustrating each diffuser component of the turbochargers illustrated in FIG. 2A , FIG. 3A , FIG. 4A , FIG. 5A , FIG. 6A , FIG. 7A , FIG. 8A , and FIG.
  • FIG. 9A in which (a) is a sectional side view of the diffuser component and (b) is a perspective view of the diffuser component.
  • FIG. 4C is a view for describing the assembling state of an insert component, a snap ring, and the diffuser component in the turbocharger illustrated in FIG. 4A .
  • FIG. 5C is a view for describing the assembling state of an insert component, a snap ring, and the diffuser component in the turbocharger illustrated in FIG. 5A .
  • FIG. 6C is a view for describing the assembling state of an insert component, a snap ring, and the diffuser component in the turbocharger illustrated in FIG. 6A .
  • the turbocharger 100 in the turbocharger 100 according to at least one embodiment of this invention, at least an insert component 6, a snap ring 8, and a diffuser component 9 in addition to the thrust plate 4 described above are accommodated in the bearing housing 106.
  • the thrust plate 4 is configured to support the rotation shaft 2 in the axial direction.
  • the thrust plate 4 is an annular plate-shaped component having an insertion hole 4A through which the rotation shaft 2 is inserted.
  • the thrust plate 4 is accommodated in the bearing housing 106 in a state in which one surface 4a of the thrust plate 4 is in abutment with a side surface of the protruding wall portion 106A of the bearing housing 106.
  • a first thrust collar 3A and a second thrust collar 3B located at a position closer to an end portion of the bearing housing 106 on one side thereof (the end portion on the side connected to the compressor housing 104) than a position of the first thrust collar 3A are mounted on the rotation shaft 2.
  • the first thrust collar 3A and the second thrust collar 3B respectively have cylindrical collar main body portions 3A1 and 3B1 and large-diameter portions 3A2 and 3B2 formed to have diameters larger than those of the collar main body portions 3A1 and 3B1, and are mounted on the outer periphery of the rotation shaft 2 so as to be rotatable with the rotation shaft 2.
  • the collar main body portion 3A1 of the first thrust collar 3A is inserted in the insertion hole 4A in the thrust plate 4.
  • the thrust plate 4 is accommodated in a recessed portion formed between the large-diameter portion 3A2 of the first thrust collar 3A and the large-diameter portion 3B2 of the second thrust collar 3B.
  • the thrust plate 4 is configured to be in sliding contact with the large-diameter portion 3A2 of the first thrust collar 3A and the large-diameter portion 3B2 of the second thrust collar 3B to support the rotation shaft 2 in the axial direction.
  • the insert component 6 is accommodated in the bearing housing 106 at a position closer to the end portion of the bearing housing 106 on one side thereof than a position of the thrust plate 4 in the axial direction of the rotation shaft 2.
  • the insert component 6 is configured to retain the thrust plate 4 between the insert component 6 and the protruding wall portion 106A of the bearing housing 106.
  • the insert component 6 includes an annular plate-shaped component having an insertion hole 6C.
  • the main body portion 3B1 of the second thrust collar 3B mounted on the outer periphery of the rotation shaft 2 is inserted in the insertion hole 6C.
  • the radially outer portion of the insert component 6 has substantially the same size as the radially inner portion of the bearing housing 106.
  • the outer peripheral surface of the insert component 6 is configured to come into abutment with the inner peripheral wall surface 106a of the bearing housing 106, and the inner peripheral surface of the insert component 6 is configured to be in sliding contact with the outer peripheral surface of the main body portion 3B1 of the second thrust collar 3B.
  • An annular seal groove is formed in the inner peripheral wall surface 106a of the bearing housing 106 positioned on the outer peripheral side of the insert component 6.
  • An annular seal component 7 such as an O ring is placed in the seal groove.
  • an oil deflector 5 is placed between the thrust plate 4 and the insert component 6.
  • the oil deflector 5 is a component configured to prevent the lubricant oil supplied to the thrust plate 4 from leaking out to the compressor impeller 105 side, and is an annular plate-shaped component made of a metallic plate, for example.
  • the oil deflector 5 is fixed in the bearing housing 106 by sandwiching a part of the outer peripheral edge thereof between the thrust plate 4 and the insert component 6.
  • the snap ring 8 is inserted in a first circumferential groove 81 formed in the inner peripheral wall surface 106a of the bearing housing 104, to thereby fix the insert component 6 in a state in which the insert component 6 is pressed against the thrust plate 4.
  • the diffuser component 9 has a diffuser surface 91a extending along the direction orthogonal to the axis of the rotation shaft 2 between the inner peripheral wall surface 106a of the end portion of the bearing housing 106 on one side thereof and an outer peripheral edge 105a of the compressor impeller 105.
  • the diffuser surface 91a is formed with the same width in the circumferential direction.
  • a gap S between the outer peripheral edge 105a of the compressor impeller 105 and the inner peripheral wall surface 106a of the end portion of the bearing housing 106 on one side thereof is filled with the diffuser surface 91a of the diffuser component 9 described above, and hence the intake air flowing through the diffuser flow path 112 can be prevented from flowing into the gap S to enhance the compression efficiency of the turbocharger 100.
  • the radially outer portion of the compressor impeller 105 is smaller than the radially inner portion of the end portion of the bearing housing 106 on one side thereof.
  • the gap S is formed between the inner peripheral wall surface 106a of the end portion of the bearing housing 106 on one side thereof and the outer peripheral edge 105a of the compressor impeller 105.
  • the size of the gap S is from 2% to 30% of an internal radius R of the end portion of the bearing housing 106 on one side thereof.
  • the gap S as above is formed in a flow path surface defining the diffuser flow path 112
  • the intake air flowing through the diffuser flow path 112 flows into the gap S to cause a large pressure loss.
  • the decrease in the compression efficiency of the turbocharger 100 due to the intake air flowing into the gap S can be prevented by filling the gap S with the diffuser surface 91a of the diffuser component 9 described above.
  • the bearing housing and the components accommodated in the bearing housing can be used in common for the turbocharger of the related-art.
  • FIG. 10 is an enlarged sectional side view illustrating an insert component according to one embodiment of this invention.
  • FIG. 2A , FIG. 3A , FIG. 4A , FIG. 5A , FIG. 6A , FIG. 7A , FIG. 8A , FIG. 9A and the enlarged view of FIG.
  • the insert component 6 includes an inner peripheral portion 6A including an inner peripheral-side wall portion 61 extending along the direction orthogonal to the axis of the rotation shaft 2, and an outer peripheral portion 6B including an outer peripheral-side wall portion 62 extending along the direction orthogonal to the axis of the rotation shaft 2 at a position farther from the end portion of the bearing housing 106 on one side thereof than a position of the inner peripheral-side wall portion 61 and a protruding portion 63 protruding from the outer peripheral-side wall portion 62 toward the thrust plate 4.
  • the snap ring 8 is configured to be positioned on the outer peripheral side of the inner peripheral portion 6A of the insert component 6 and configured to come into abutment with the outer peripheral-side wall portion 62 of the insert component 6 in a state in which the snap ring 8 is inserted in the first circumferential groove 81.
  • the diffuser component 9 is configured to be positioned on the outer peripheral side of the inner peripheral portion 6A of the insert component 6.
  • the protruding portion 63 of the insert component 6 protrudes from an outer peripheral end portion of the outer peripheral-side wall portion 62.
  • An outer peripheral surface 63a of the protruding portion 63 is in abutment with the inner peripheral wall surface 106a of the bearing housing 106.
  • the distal end of the protruding portion 63 is in abutment with an outer peripheral end portion of another surface 4b of the thrust plate 4.
  • a step portion 63b configured to come into abutment with an outer peripheral end portion of the oil deflector 5 is formed in the distal end of the protruding portion 63.
  • the inner peripheral portion 61 of the insert component 6 includes an extension portion 64 extending from an inner peripheral end portion of the inner peripheral-side wall portion 61 toward the thrust plate 4 along the axial direction of the rotation shaft 2.
  • a connection portion 65 configured to connect the inner peripheral portion 6A and the outer peripheral portion 6B to each other is formed between the inner peripheral portion 6A and the outer peripheral portion 6B.
  • the outer peripheral-side wall portion 62 of the outer peripheral portion 6B is at a position farther from the end portion of the bearing housing 106 on one side thereof than a position of the inner peripheral-side wall portion 61 of the inner peripheral portion 6A.
  • the outer peripheral-side wall portion 62 is positioned closer to the thrust plate 4 than the inner peripheral-side wall portion 61.
  • a space is formed between the inner peripheral portion 6A on the outer peripheral side thereof and the inner peripheral wall surface 106a of the bearing housing 106.
  • the snap ring 8 is configured to come into abutment with the outer peripheral-side wall portion 62 of the insert component 6 in a state in which the snap ring 8 is inserted in the first circumferential groove 81. As a result, the pressing force transmitted from the snap ring 8 to the insert component 6 can be efficiently transmitted to the thrust plate 4 via the protruding portion 63 protruding from the outer peripheral-side wall portion 62.
  • the diffuser component 9 includes a plate-shaped diffuser portion 91 having the diffuser surface 91a, and a plate-shaped outer peripheral-side plate portion 92 extending from an outer peripheral end portion of the diffuser portion 91 along the axial direction of the rotation shaft 2.
  • the outer peripheral-side plate portion 92 is configured to come into abutment with the inner peripheral wall surface 106a of the bearing housing 106 along the axial direction of the rotation shaft 2.
  • the outer peripheral-side plate portion 92 of the diffuser component 9 is configured to come into abutment with the inner peripheral wall surface 106a of the bearing housing 106 along the axial direction of the rotation shaft 2.
  • the accuracy of positioning the diffuser component 9 in the direction orthogonal to the axis of the rotation shaft 2 can be enhanced.
  • the insert component 6 includes a projecting portion 66 protruding from an outer peripheral end surface 61a of the inner peripheral portion 6A to the outer peripheral side.
  • the diffuser component 9 includes a plate-shaped inner peripheral-side plate portion 93 extending from an inner peripheral end portion of the diffuser portion 91 toward the inner peripheral portion 6A of the insert component 6.
  • an inner peripheral end 93a of the inner peripheral-side plate portion 93 is configured to be positioned farther from the end portion of the bearing housing 106 on one side thereof than the projecting portion 66 in the axial direction of the rotation shaft 2, and positioned closer to the rotation shaft 2 than an outer peripheral end 66a of the projecting portion 66 in the direction orthogonal to the axis of the rotation shaft 2.
  • the inner peripheral-side plate portion 93 includes a horizontal portion 931 extending from the inner peripheral end portion of the diffuser portion 91 along the axial direction of the rotation shaft 2 and a vertical portion 932 extending from an end portion of the horizontal portion 931 along the direction orthogonal to the axis of the rotation shaft 2.
  • the projecting portion 66 forms an annular shape continuously extending in the circumferential direction.
  • the diffuser component 9 when the diffuser component 9 is about to fall out of the opening in the end portion of the bearing housing 106 on one side thereof, the inner peripheral-side plate portion 93 of the diffuser component 9 is caught by the projecting portion 66 of the insert component 6. As a result, the diffuser component 9 can be prevented from falling out.
  • the radially outer portion of the diffuser component 9 is formed to be larger than the radially inner portion of the end portion of the bearing housing 106 on one side thereof. As illustrated in FIG. 2A and FIG. 2B , the diffuser component 9 is press fitted in the bearing housing 106, to thereby be fixed in the bearing housing 106.
  • the radially outer portion of the diffuser component 9, specifically, the radially outer portion of the outer peripheral-side plate portion 92 in a state before the diffuser component 9 is press fitted in the bearing housing 106 is formed to be slightly larger than the radially inner portion of the end portion of the bearing housing 106 on one side thereof.
  • the diffuser component 9 can be fixed in the bearing housing 106 through a simple structure in which the diffuser component 9 is simply press fitted in the bearing housing 106.
  • the radially inner portion of the diffuser component 9 is formed to be smaller than the radially outer portion of the outer peripheral end surface 61a of the inner peripheral portion 6A of the insert component 6. As illustrated in FIG. 2A and FIG. 2B , the diffuser component 9 is fitted with the outer peripheral end surface 61a of the inner peripheral portion 6A of the insert component 6, to thereby be fixed in the bearing housing 106.
  • the radially inner portion of the diffuser component 9, specifically, the radially inner portion of the inner peripheral-side plate portion 93 in a state before the diffuser component 9 is fitted with the outer peripheral end surface 61a of the inner peripheral portion 6A of the insert component 6 is formed to be slightly smaller than the radially outer portion of the outer peripheral end surface 61a of the inner peripheral portion 6A of the insert component 6.
  • the diffuser component 9 is inserted in the bearing housing 106 from the opening in the end portion of the bearing housing 106 on one side thereof, and the inner peripheral-side plate portion 93 of the diffuser component 9 is fitted with the outer peripheral end surface 61a of the inner peripheral portion 6A of the insert component 6, to thereby fix the diffuser component 9 to the inside of the bearing housing 106.
  • the diffuser component 9 can be fixed in the bearing housing 106 through a simple structure in which the diffuser component 9 is simply fitted with the outer peripheral end surface 61a of the inner peripheral portion 6A of the insert component 6.
  • the diffuser component 9 is configured to come into abutment, at the distal end of the outer peripheral-side plate portion 92, with the snap ring 8 inserted in the first circumferential groove 81.
  • the diffuser component 9 is configured to be at a position suitable for the diffuser surface 91a of the diffuser portion 91 to define the diffuser flow path 112 in a state in which the distal end of the outer peripheral-side plate portion 92 is in abutment with the snap ring 8 inserted in the first circumferential groove 81.
  • the diffuser component 9 when the diffuser component 9 is inserted in the bearing housing 106 from the opening in the end portion of the bearing housing 106 on one side thereof, the diffuser component 9 can be easily positioned in the axial direction of the rotation shaft 2.
  • a second circumferential groove 99 is formed in the inner peripheral wall surface 106a of the bearing housing 106 at a position closer to the end portion of the bearing housing 106 on one side thereof than a position of the first circumferential groove 81 in the axial direction of the rotation shaft 2.
  • the diffuser component 9 includes a plate-shaped insert plate portion 94 extending from the outer peripheral-side plate portion 92 to the outer peripheral side. The insert plate portion 94 is configured to be inserted in the second circumferential groove 99.
  • the insert plate portion 94 extends from the distal end of the outer peripheral-side plate portion 92 along the direction orthogonal to the axis of the rotation shaft 2.
  • the position of the insert plate portion 94 in the axial direction of the rotation shaft 2 is closer to the end portion of the bearing housing 106 on one side thereof than the vertical portion 932 of the inner peripheral-side plate portion 93.
  • the diffuser component 9 can be fixed in the bearing housing 106 through a simple structure in which the insert plate portion 94 of the diffuser component 9 is simply inserted in the second circumferential groove 99.
  • the dimension tolerance of the diffuser component 9 on the outer peripheral side can be set to be loose.
  • the second circumferential groove 99 is formed over the entire periphery of the inner peripheral wall surface 106a of the bearing housing 106.
  • the insert plate portion 94 is configured to be inserted in the second circumferential groove 99 over the entire periphery of the inner peripheral wall surface 106a of the bearing housing 106.
  • the diffuser component 9 can be reliably fixed in the bearing housing 106 because the insert plate portion 94 of the diffuser component 9 is inserted in the second circumferential groove 99 over the entire periphery of the inner peripheral wall surface 106a of the bearing housing 106.
  • the first circumferential groove 81 is formed over the entire periphery of the inner peripheral wall surface 106a of the bearing housing 106.
  • the snap ring 8 has a spaced section 82 formed by separating end portions 8a and 8b of an arc shape from each other. Specifically, the snap ring 8 is formed to have a C-shape in which a part of the annular shape is cut out.
  • the outer peripheral-side plate portion 92 of the diffuser component 9 includes a first outer peripheral-side plate portion 921 and a second outer peripheral-side plate portion 922.
  • the second outer peripheral-side plate portion 922 is formed at a position different from that of the first outer peripheral-side plate portion 921 in the circumferential direction and has an extending length that is shorter than that of the first outer peripheral-side plate portion 921.
  • the insert plate portion 94 of the diffuser component 9 includes a first insert plate portion 941 extending from the first outer peripheral-side plate portion 921 to the outer peripheral side and a second insert plate portion 942 extending from the second outer peripheral-side plate portion 922 to the outer peripheral side.
  • the second insert plate portion 942 is configured to be inserted in the second circumferential groove 99, and the first insert plate portion 941 is configured to be inserted in the first circumferential groove 81 at the spaced section 82 of the snap ring 8 inserted in the first circumferential groove 81.
  • the length of the first insert plate portion 941 in the circumferential direction is shorter than the distance between one end portion 8a and the other end portion 8b of the snap ring 8.
  • the length of the second insert plate portion 942 in the circumferential direction is not particularly limited, but is substantially the same length as the length of the circumferential direction of the first insert plate portion 941 in the embodiment illustrated in the drawings.
  • the second circumferential groove 99 is formed in the circumferential direction over at least a length equal to or longer than the length of the second insert plate portion 942 in the circumferential direction.
  • the first insert plate portion 941 is inserted in a part of the first circumferential groove 81 in which the snap ring 8 is not inserted (a gap 82 of the snap ring 8).
  • the second insert plate portion 942 is inserted in the second circumferential groove 99.
  • the part of the bearing housing 106 to be processed can be kept at a minimum by effectively utilizing the first circumferential groove 81 formed for inserting the snap ring 8 therein.
  • the diffuser component 9 can be reliably fixed in the bearing housing 106 by inserting the second insert plate portion 942 in the second circumferential groove 99 in addition to inserting the first insert plate portion 941 in the first circumferential groove 81.
  • the first insert plate portion 941 and the second insert plate portion 942 are formed at positions opposed to each other in the circumferential direction.
  • the first insert plate portion 941 and the second insert plate portion 942 are formed at positions opposed to each other in the circumferential direction.
  • the diffuser component 9 can be more reliably fixed to the inside of the bearing housing 106 because the diffuser component 9 can be supported by two places opposed to each other in the circumferential direction.
  • the diffuser component 9 includes a plate-shaped cylindrical plate portion 95 extending from the inner peripheral end portion of the diffuser portion 91 toward the insert component 6 along the axial direction of the rotation shaft 2.
  • the insert component 6 has a projecting portion 67 protruding from the outer peripheral end surface 61a of the inner peripheral portion 6A to the outer peripheral side, and at least one projecting portion 67 is formed in the circumferential direction or the projecting portion 67 is formed in plurality at intervals in the circumferential direction.
  • a recessed portion 951 or a slit 952 in which the projecting portion 67 is inserted when the cylindrical plate portion 95 is fitted with the outer peripheral end surface 61a of the inner peripheral portion 6A of the insert component 6 is formed in an inner peripheral surface 95a of the cylindrical plate portion 95 along the axial direction of the rotation shaft 2.
  • the radially inner portion of the diffuser component 9, specifically, the radially inner portion of the cylindrical plate portion 95 in a state before the diffuser component 9 is fitted with the outer peripheral end surface 61a of the inner peripheral portion 6A of the insert component 6 is formed to be slightly smaller than the radially outer portion of the outer peripheral end surface 61a of the inner peripheral portion 6A of the insert component 6.
  • the radially outer portion of the outer peripheral end surface 61a of the inner peripheral portion 6A of the insert component 6 is formed to be larger than the radially outer portion of the compressor impeller 105.
  • the diffuser component 9 is inserted in the bearing housing 106 from the opening in the end portion of the bearing housing 106 on one side thereof, and the cylindrical plate portion 95 of the diffuser component 9 is fitted with the outer peripheral end surface 61a of the inner peripheral portion 6A of the insert component 6, to thereby fix the diffuser component 9 to the inside of the bearing housing 106.
  • the cylindrical plate portion 95 of the diffuser component 9 is fitted with the outer peripheral end surface 61a of the inner peripheral portion 6A of the insert component 6 in addition to inserting the first insert plate portion 941 in the first circumferential groove 81 and inserting the second insert plate portion 942 in the second circumferential groove 99.
  • the diffuser component 9 can be more reliably fixed to the inside of the bearing housing 106.
  • the recessed portion 951 or the slit 952 in which the projecting portion 67 is inserted when the cylindrical plate portion 95 is fitted with the outer peripheral end surface 61a of the inner peripheral portion 6A of the insert component 6 is formed in the inner peripheral surface 95a of the cylindrical plate portion 95 along the axial direction of the rotation shaft 2.
  • the diffuser component 9 can be easily positioned in the circumferential direction by inserting the diffuser component 9 in the bearing housing 106 along the axial direction of the rotation shaft 2 so that the projecting portion 67 is inserted in the recessed portion 951 or the slit 952.
  • the upper part of the view illustrates a state in which the projecting portion 67 is inserted in the recessed portion 951 formed in the inner peripheral surface 95a of the cylindrical plate portion 95
  • the lower part of the view illustrates a state in which the projecting portion 67 is inserted in the slit 952 formed in the inner peripheral surface 95a of the cylindrical plate portion 95.
  • the diffuser component 9 includes a plate-shaped horizontal plate portion 96 extending from the inner peripheral end portion of the diffuser portion 91 toward the insert component 6 along the axial direction of the rotation shaft 2.
  • a bulged portion 961 bulging more than other portions of the horizontal plate portion 96 is formed on the distal end of the horizontal plate portion 96.
  • a fitting groove 621 with which the distal end of the horizontal plate portion 96 can be fitted is formed in the outer peripheral-side wall portion 62 of the insert component 6.
  • the horizontal plate portion 96 is formed to be an annular shape continuous in the circumferential direction, but the horizontal plate portion 96 may be formed in only a part of the circumferential direction.
  • the bulged portion 961 is formed by bending the distal end of the horizontal plate portion 96 into a curve.
  • the shape and the processing method of the bulged portion 961 are not limited thereto.
  • the bulged portion 961 only needs to have a shape bulging more than other portions of the horizontal plate portion 96 so as to be able to be fitted with the fitting groove 621.
  • the diffuser component 9 can be fixed in the bearing housing 106 through a simple structure in which the distal end of the horizontal plate portion 96 of the diffuser component 9 is simply fitted with the fitting groove 621 in the insert component 6.
  • the diffuser component 9 includes a plate-shaped component formed by bending a metallic plate.
  • the diffuser component 9 can be formed by a simple method of simply bending a metallic plate. Furthermore, the surface roughness of a metallic plate is higher than that of a casting and the like. As a result, according to the embodiment as above, the pressure loss in the diffuser flow path 112 can be reduced because the diffuser portion 91 defining the diffuser flow path 112 is made of a metallic plate.
  • a screw hole 97 with which a screw component 10 can be threadedly engaged is formed in the diffuser portion 91 of the diffuser component 9.
  • a screw hole 622 with which the screw component 10 can be threadedly engaged is formed in the outer peripheral-side wall portion 62 of the insert component 6.
  • the diffuser component 9 is configured to be fastened with the insert component 6 by threadedly engaging the screw component 10 with the screw hole 97 in the diffuser component 9 and the screw hole 622 in the insert component 6 from the diffuser surface 91a of the diffuser component 9.
  • the diffuser portion 91 of the diffuser component 9 has a thickness needed for the formation of the screw hole 97.
  • the diffuser component 9 as above is made of cast metal or heat-resistant resin.
  • the diffuser component 9 can be fixed in the bearing housing 106 through a simple structure in which the diffuser component 9 is simply threadedly engaged with the insert component 6 by the screw component 10.
  • a screw groove 106b having a predetermined length is formed in the inner peripheral wall surface 106a of the bearing housing 106 from the end portion of the bearing housing 106 on one side thereof along the axial direction of the rotation shaft 2.
  • the diffuser component 9 is formed into an annular shape, and a screw thread 98 that can threadedly engage with the screw groove 106b is formed in the outer peripheral surface of the diffuser component 9.
  • the diffuser component 9 can be fixed in the bearing housing 106 through a simple structure in which the outer peripheral surface of the diffuser component 9 and the inner peripheral wall surface 106a of the bearing housing 106 are simply threadedly engaged with each other.
  • turbocharger 100 is a turbocharger
  • turbocharger of this invention is not limited thereto.
  • the turbocharger of this invention may be, for example, an electric compressor in which a rotation shaft rotates by a motor, or a mechanical supercharger in which a rotation shaft rotates by power transmitted from a crankshaft or the like.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)
EP15881914.4A 2015-02-09 2015-02-09 Compresseur de suralimentation Active EP3258080B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/JP2015/053529 WO2016129039A1 (fr) 2015-02-09 2015-02-09 Compresseur de suralimentation

Publications (3)

Publication Number Publication Date
EP3258080A1 true EP3258080A1 (fr) 2017-12-20
EP3258080A4 EP3258080A4 (fr) 2018-01-24
EP3258080B1 EP3258080B1 (fr) 2019-06-19

Family

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EP15881914.4A Active EP3258080B1 (fr) 2015-02-09 2015-02-09 Compresseur de suralimentation

Country Status (5)

Country Link
US (1) US10844902B2 (fr)
EP (1) EP3258080B1 (fr)
JP (1) JP6396512B2 (fr)
CN (1) CN107208544B (fr)
WO (1) WO2016129039A1 (fr)

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US10731546B2 (en) * 2017-02-06 2020-08-04 Borgwarner Inc. Diffuser in wastegate turbine housings
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US11067131B2 (en) * 2018-06-07 2021-07-20 Borg Warner Inc. Anti-rotation assembly and bearing housing assembly including the same

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Also Published As

Publication number Publication date
EP3258080A4 (fr) 2018-01-24
EP3258080B1 (fr) 2019-06-19
WO2016129039A1 (fr) 2016-08-18
JP6396512B2 (ja) 2018-09-26
JPWO2016129039A1 (ja) 2017-08-31
CN107208544B (zh) 2020-03-03
US20180238383A1 (en) 2018-08-23
US10844902B2 (en) 2020-11-24
CN107208544A (zh) 2017-09-26

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